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<title cf:type="text"><![CDATA[Editorial department of the Journal of National University of Defense Technology -->材料科学与工程·电子科学与技术]]></title>
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<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Prediction of creep performance for multiple launch rocket canister under long-term storage]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202005009]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[In order to investigate the creep performance of multi-barrel rocket weapon launch canister under long-term storage, uniaxial tensile creep test was carried out on composite laminate and the creep constitutive model parameters of single layer in the main directions were obtained. The finite element method and the user-defined material subroutine were used to establish long-term storage numerical analysis model of launch canister. Creep deformation of the bottom launch canister after 15 years storage was predicted. Taking the stored launch canister as initial state, the dynamic simulation model of rocket-tube coupling was built, and the influence of creep on rocket launching process was further investigated. Simulation results show that the change of the parallelism of the director and the flatness of the bottom surface of launch canister caused by creep are smaller than the specified values of technical indicators. The maximum residual deformation of director bundle is saddle-shaped in three-dimensional space, and the deformations of the middle position directors for upper and lower rows are largest, while that of the middle position directors for left and right columns are smallest. Creep deformation of the director reduces the clearance between rocket and director, increases the dynamic contact collision force and lessens the off-track velocity of rocket.]]></description>
<pubDate>2020/10/21 0:00:00</pubDate>
<category><![CDATA[材料科学与工程·电子科学与技术]]></category>
<author><![CDATA[SUN Tongsheng, YU Cungui, QIN Yuzheng, WANG Qi]]></author>
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<atom:name>SUN Tongsheng, YU Cungui, QIN Yuzheng, WANG Qi</atom:name>
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<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Cu-based diamond-like carbon film with high adhesion prepared by pulsed laser deposition]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202005010]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[Improvement for the adhesive property of the DLC (diamond-like carbon) film on the protected substrate has obvious value in the actual application, and the reason for the validity of the Cu-based multi-layer DLC film designed in our former research was analyzed in the view of the micro-theory. Then, in order to optimize the structure of the multi-layer film and improve its performance in the practical application, the influences of the thickness ratio between the DLC layer and SiC layer in the periodic layer on the adhesion property, nano-hardness and wear property were studied. The results of the nano-scratch and nano-indentation tests show that the adhesive property and nano-hardness of the Cu-based multi-layer DLC film decreased and its nano-hardness increased, respectively, while the thickness ratio was maintained in the increasing state. Critical load of the multi-layer DLC film on the Cu substrate could approach that of the single-layer DLC film with the thickness of 400 nm on the Si substrate, when the thickness ratio was below 2.3. Meanwhile, the wear property of the Cu-based multi-layer DLC film was approximately close to that of the pure DLC film.]]></description>
<pubDate>2020/10/21 0:00:00</pubDate>
<category><![CDATA[材料科学与工程·电子科学与技术]]></category>
<author><![CDATA[LU Yimin, HUANG Guojun, MI Chaowei, XI Lin, WANG Sai, CAO Haiyuan, CHENG Yong]]></author>
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<atom:name>LU Yimin, HUANG Guojun, MI Chaowei, XI Lin, WANG Sai, CAO Haiyuan, CHENG Yong</atom:name>
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<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Energy absorption mechanism of filament wound composite core cylinder under high strain rate compressive load]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202005011]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[In order to investigate the damage modes and energy absorption mechanism of the filament wound composite core cylinder under high strain rate impact compression load, the numerical simulation analysis and experimental test verification were carried out by using the ABAQUS finite element software and the Hopkinson bar testing machine. The analysis of the mechanical response characteristics and damage modes show that the energy absorbing element has typical elastic-plastic response characteristics under the high rate impact compression loading. The inner core material mainly produces compression plastic damage, while the surface composite material produces tensile fracture damage along the hoop direction. The study results show that this type of energy absorbing element has excellent compression and energy absorption characteristics, and can achieve the impact protection and buoyancy reserve requirements of the underwater structure platform.]]></description>
<pubDate>2020/10/21 15:50:32</pubDate>
<category><![CDATA[材料科学与工程·电子科学与技术]]></category>
<author><![CDATA[ZHOU Xiaosong, MEI Zhiyuan]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>ZHOU Xiaosong, MEI Zhiyuan</atom:name>
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<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202005011]]></guid><cfi:id>4</cfi:id><cfi:read>true</cfi:read></item>
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<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Analysis and suppressing method for the operating range ambiguity of torpedo electromagnetic fuze]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202005012]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[Starting from the basic principle of the vertical configuration of the receiving and transmitting coils of torpedo electromagnetic fuze, the ambiguity of operating range caused by the double receiving coils located on the torpedo axis and deviating from the torpedo axis were analyzed respectively. For the first case, the modulo operation of the double receiving coils was proposed to eliminate the ambiguity of the operating distance; for the second case, a pair of coils was appended to the symmetrical position and the output signal of the symmetrical position coil was averaged, then the modulo operation was taken to eliminate the ambiguity of the operating range. Simulation results show that the method can effectively eliminate the ambiguity of the operating range and improve the operating range of the electromagnetic fuze.]]></description>
<pubDate>2020/10/21 15:50:32</pubDate>
<category><![CDATA[材料科学与工程·电子科学与技术]]></category>
<author><![CDATA[TANG Bo, TAN Siwei, ZHANG Jingyuan]]></author>
<atom:author xmlns:atom="http://www.w3.org/2005/Atom">
<atom:name>TANG Bo, TAN Siwei, ZHANG Jingyuan</atom:name>
</atom:author>
<guid><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202005012]]></guid><cfi:id>3</cfi:id><cfi:read>true</cfi:read></item>
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<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Design of radial line continuous transverse stub antenna for high-power microwave applications]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202005013]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[In order to realize the directed radiating of Ku-band HPM (high-power microwave), a RL-CTSA (radial line continuous transverse stub antenna) was proposed. The antenna was fed by circularly polarized coaxial TE<sub>11</sub> mode and radiated by a concentric CTS (continuous transverse stub) array after the wave propagation through a double-layered radial line waveguide. The interspace between adjacent stubs along radial direction was equal to one guide wavelength, a shorting pin was located at the end of the upper radial line waveguide and the space between the pin′s surface and the innermost CTS radiator′s center was half a guide wavelength. As a result, the HPM-RL-CTSA works on standing wave. An antenna prototype with a height of 80 mm and an aperture radius of 285 mm operating at 14.25 GHz has been designed, which has a gain of 35.3 dBi, reaching an aperture efficiency of 47%. The reflectance of this antenna is less than -25 dB and the radiation efficiency is more than 99.0%. The simulated results indicate that this antenna has a power handing capacity of more than 1 GW.]]></description>
<pubDate>2020/10/21 15:50:32</pubDate>
<category><![CDATA[材料科学与工程·电子科学与技术]]></category>
<author><![CDATA[SUN Yunfei, HE Juntao, YUAN Chengwei, ZHANG Qiang, ZHANG Zehai]]></author>
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<atom:name>SUN Yunfei, HE Juntao, YUAN Chengwei, ZHANG Qiang, ZHANG Zehai</atom:name>
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<title xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="text"><![CDATA[Research on temperature of electromagnetic rail launcher based on gray model]]></title>
<link><![CDATA[http://journal.nudt.edu.cn/gfkjdxxben/article/abstract/202005014]]></link>
<description xmlns:cf="http://www.microsoft.com/schemas/rss/core/2005" cf:type="html"><![CDATA[During the electromagnetic launch process, the temperature of the rail is affected by many factors and it is difficult to analyze some factors accurately. Based on this, the gray system was used to study the temperature of the electromagnetic launcher. In order to obtain the experimental data needed for the gray model, the electromagnetic launcher data collection system was built, and such data as the current, the rail temperature, the launch speed and other factors concerned were collected. Due to the limitations of measuring instruments, the ANSYS finite-element simulation was adopted to correct the measured rail temperature data to obtain the inner surface temperature of the rail. Based on the classical GM(1,N) and Simpson formula, an improved gray model was proposed, and the rail temperature was studied by this method. The same energy level test was conducted to discuss the contribution of temperature rise of various factors at different locations. The conclusion provides a reference and basis for further research on the temperature of the rail.]]></description>
<pubDate>2020/10/21 15:50:32</pubDate>
<category><![CDATA[材料科学与工程·电子科学与技术]]></category>
<author><![CDATA[LI Songcheng, LU Junyong, CHENG Long, WU Yiting]]></author>
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<atom:name>LI Songcheng, LU Junyong, CHENG Long, WU Yiting</atom:name>
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